Bank-to-turn Missile Autopilot Design Based on Linear Quadratic Regulator Controller

WANG  Guangshan; WANG  Jiang

doi:10.15892/j.cnki.djzdxb.2018.03.018

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2018, Vol. 38 ›› Issue (3) : 75-78,83. DOI: 10.15892/j.cnki.djzdxb.2018.03.018

MISSILES AND GUIDANCE TECHNOLOGY

Bank-to-turn Missile Autopilot Design Based on Linear Quadratic Regulator Controller

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2018, 38(3): 75-78,83 https://doi.org/10.15892/j.cnki.djzdxb.2018.03.018

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Received	Published
2017-06-29	2018-06-20
Issue Date
2025-05-30

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